Modulation of Aerodynamic Angles for Optimal Mars Descent Trajectory using Indirect Approach

Author(s):  
Megh Bhatnagar ◽  
R. V. Ramanan
2007 ◽  
Author(s):  
Josh Davis ◽  
Amanda D. Angie ◽  
Mary Shane Connelly ◽  
Greg Ruark ◽  
Jason H. Hill
Keyword(s):  

Author(s):  
Guilherme Barufaldi ◽  
Marcus Victor ◽  
Luiz Carlos Sandoval Góes ◽  
ROBERTO GIL ANNES DA SILVA

2012 ◽  
Vol 54 (5-6) ◽  
pp. 745-753 ◽  
Author(s):  
A. Tumino ◽  
C. Spitaleri ◽  
S. Cherubini ◽  
M. Gulino ◽  
M. La Cognata ◽  
...  

2013 ◽  
Vol 671-674 ◽  
pp. 1614-1618 ◽  
Author(s):  
Pavel A. Akimov

This paper is devoted to so-called indirect discrete-continual boundary element method of structural analysis. Operational formulation of the problem is given. Using fundamental operational relations of indirect approach after construction of corresponding fundamental matrix-function in a special form convenient for problems of structural mechanics and its application resolving set of differential equations with operational coefficients is obtained. The discrete-continual design model for structures with constant physical and geometrical parameters in one direction is offered on the basis of so-called discrete-continual boundary elements. Basic pseudodifferential operators are approximated discretely by Fourier series. Fourier transformations and Wavelet analysis can be applied as well.


2010 ◽  
Vol 22 (3) ◽  
pp. 295-304 ◽  
Author(s):  
V. Lorieto ◽  
S. Ghione ◽  
C. Viera

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